首页> 外国专利> A method for the production of a turbine blade made of ceramic matrix composite material, use for a turbine blade made of ceramic matrix composite material and turbine blade made of ceramic matrix composite material

A method for the production of a turbine blade made of ceramic matrix composite material, use for a turbine blade made of ceramic matrix composite material and turbine blade made of ceramic matrix composite material

机译:一种由陶瓷基复合材料制成的涡轮叶片的生产方法,用于由陶瓷基复合材料制成的涡轮叶片和由陶瓷基复合材料制成的涡轮叶片

摘要

There are a method for producing a turbine blade made of ceramic matrix composite material, a use for a turbine blade made of ceramic matrix composite material and a turbine blade made of ceramic matrix composite material. The method comprises providing a blade preform, which has a dovetail, hollow space, wherein the dovetail hollow space of a dovetail shaft of the blade preform is enclosed, positioning of a dovetail insert within the hollow space, then form the turbine blade made of ceramic matrix composite material in a furnace. The insert has a geometry which is arranged so that, within a dovetail hollow space of the turbine blade made of ceramic matrix composite material, of a blade preform to be used or of two. The insert is a foamed material or a plurality of ceramic matrix composite material layers. The turbine blade made of ceramic matrix composite material has a dovetail shaft and of a dovetail, hollow space, which is surrounded by the dovetail shaft. The dovetail hollow space to receive an insert is disposed and arranged.
机译:有一种用于制造由陶瓷基复合材料制成的涡轮叶片的方法,一种用于由陶瓷基复合材料制成的涡轮叶片和由陶瓷基复合材料制成的涡轮叶片的用途。该方法包括:提供具有燕尾形空心空间的叶片预型件,其中,将叶片预型件的燕尾轴的燕尾形空心空间封闭,将燕尾形插入物定位在该空心空间内,然后形成由陶瓷制成的涡轮机叶片炉中的基体复合材料。插入件具有这样的几何形状,该几何形状布置成使得在由陶瓷基复合材料制成的涡轮叶片的燕尾形中空空间内,可以使用一个或两个叶片预制件。插入物是泡沫材料或多个陶瓷基复合材料层。由陶瓷基复合材料制成的涡轮叶片具有燕尾轴和燕尾的中空空间,该空间被燕尾轴围绕。设置并布置了用于容纳插入件的燕尾形空腔。

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